Aircraft Parametric 3D Modeling and Panel Code Analysisfor Conceptual Deisgn
2008 (English)In: International Council of the Aeronautical Sciencess ICAS, 2008: Vol. 1, Anchorage, Alaska, USA: International Council of the Aeronautical Sciences (ICAS) , 2008, 159-167 p.Conference paper (Other academic)
The ever fast growing information technology is enabling a re-definition of the early stages of aircraft design which have been restricted to mostly statistical and empirical approaches because of lengthy and costly simulation times. A novel framework is being developed at Linköping University offering greater comprehension by enabling a holistic view of the aircraft systems with a multidisciplinary analysis approach, involving a centralized easy to use interface. This paper will depict the modules involving an aerodynamic panel code solver integrated to a parametric CAD model. The connection between these tools is made fully automatic, meaning that any modification on the CAD model will with a press of button be aerodynamically analyzed in the panel solver, including re-meshing and re-writing of a input file and finally re-distributing the output file to all other modules involved in the framework.
Place, publisher, year, edition, pages
Anchorage, Alaska, USA: International Council of the Aeronautical Sciences (ICAS) , 2008. 159-167 p.
Aircraft design, Knowledge based CAD, Multidisciplinary Design, Panel Code Aerodynamic analysis
Engineering and Technology
IdentifiersURN: urn:nbn:se:liu:diva-43595Local ID: 74351ISBN: 978-1-60560-715-3OAI: oai:DiVA.org:liu-43595DiVA: diva2:264455
26th Congress of the International Council of the Aeronautical Sciences, Anchorage, Alaska, USA, September 14-19, 2008,